Piper PA-28 Cherokee 180 Checklist
Piper PA-28 Cherokee 180 · Checklist
Overview
This document is a checklist specifically for the Piper PA-28 Cherokee 180. It provides a comprehensive list of procedures and checks that pilots should perform before, during, and after flight operations. The checklist includes critical speeds, weight specifications, fuel requirements, and detailed preflight, startup, taxi, takeoff, landing, and shutdown procedures. It is designed to ensure safety and compliance with operational standards, making it an essential tool for pilots operating this aircraft model.
- Vs0: 49 KIAS, Vs1: 58 KIAS, Vr: 65-70 KIAS
- Max gross weight: 2400 lbs, Standard empty weight: 1310 lbs
- Fuel capacity: 50 gallons total, 49.75 gallons usable
- Oil capacity: 6-8 quarts, Tire pressure: 24 psi
- Throttle for takeoff: full, Rotate at 65-70 KIAS
Document
Source
Originally published by www.coyoteflight.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Checklist
- Pages
- 2
- File size
- 192 KB
- Publisher
- www.coyoteflight.com
Most owners only have the POH. Here's the essential set for the Piper PA-28 Cherokee 180.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
More Piper PA-28 Cherokee 180manuals & documents
See all 18 →- 2021 Cherokee 180 GuideChecklist
- Airworthiness Concern SheetAirworthiness Directives
- Pilot´s Operating Handbook for the Piper PA-28-140 - Cherokee Cruiser, Piper PA-28-150/160/180 - Cherokee, Piper PA-28-151 - Cherokee Warrior, Piper PA-28-161 - Cadet, Warrior II & III Equipped with TAE 125 InstallationEmergency Procedures
- Piper Cherokee 180 ChecklistChecklist
- CHEROKEE 180 OWNER'S HANDBOOKFlight Manual
- Weight and Balance DataWeight And Balance
- Piper Cherokee Owner's HandbookWeight And Balance
- PIPER CHEROKEE 180 – PA-28-180Specifications
- Pilot's Operating HandbookPilot's Operating Handbook
- Pilot's Operating HandbookPilot's Operating Handbook
- Pilot's Operating HandbookPilot's Operating Handbook
- Airplane Flight ManualFlight Manual
In this document
Speeds and Specifications
The checklist outlines key performance speeds for the Piper PA-28 Cherokee 180, including stall speeds (Vs0 at 49 KIAS, Vs1 at 58 KIAS), rotation speed (Vr between 65-70 KIAS), and climb speeds (Vx at 65 KIAS, Vy at 75 KIAS). It also lists the aircraft's standard empty weight at 1310 lbs and a maximum gross weight of 2400 lbs.
Fuel and Oil Requirements
Fuel specifications indicate a total capacity of 50 gallons, with 49.75 gallons being usable. The oil capacity is specified as 6-8 quarts. Tire pressures are also noted, with the nose and main tires requiring 24 psi.
Preflight Inspection
The preflight inspection section details checks for the right wing, nose, left wing, and empennage. Key items include verifying the security of flaps and ailerons, checking fuel quantity visually, and ensuring the engine cowling is secure and undamaged.
Engine Start Procedures
Before starting the engine, the checklist emphasizes the importance of applying brakes, setting the mixture to rich, and ensuring the throttle is open ¼ inch. The ignition switch should be set to left mag only, and the prop area must be clear before starting.
Takeoff and Climb Procedures
During takeoff, the checklist specifies that the throttle should be full, with a rotation speed of 65-70 KIAS. For initial climb-out, maintain a speed of 75 KIAS. The checklist also includes procedures for normal, short-field, and soft-field takeoffs.
Descent and Landing
For landing, the checklist advises securing seatbelts and harnesses, setting the throttle to approximately 1500 rpm, and ensuring the airspeed is between 75-80 KIAS on final approach. It also includes post-landing procedures such as retracting flaps and turning off the fuel pump.
Safety notes
- The information in this checklist is partial and should not substitute for the approved pilot’s operating handbook.
- Use of this checklist indicates that the user assumes all risk of use and consents to bear all liability associated with its use.
Full document text
Cherokee 180 Speeds (KIAS @ max gross weight) Vs0 ..................................................................49 Vs1 ..................................................................58 Vr.............................................................. 65-70 Vx ...................................................................65 Vy ...................................................................75 Va .................................................................114 Vfe ................................................................100 Vg ...................................................................75 Vno ................................................................121 Vne ................................................................148 Max Crosswind Comp ....................................17 Max Glide Distance .......... 1 NM per 1000ft AGL Specifications Standard empty weight ......................... 1310 lbs Gross weight ........................................ 2400 lbs Fuel Total ................................................. 50 gal Useable ....................................... 49.75 gal Pressure .................................... 0.5-6.0 psi Oil ........................................................... 6-8 qts Tire pressure Nose............. 24 psi (6.00x6, 4-ply or 6-ply) Main(s) ......... 24 psi (6.00x6, 4-ply or 6-ply) Gear extension (on ground) ....................... 4.5 in Cabin Dispatch status..................... signed/In-progress Hobbs & tach time ................................... record Required docs (ARROW) Airworthiness ..............................on board Registration .................................. current Radio certificates ................. for int’l flights Operating limitations ...................on board Weight and balance of A/C ........... current Control lock ............................................ remove Ignition key ................................... on dashboard Flaps ......................................................... down Avionics switch ...............................................off Master switch .................................................on Fuel gauges ............................ verify operational Exterior lights .......................... verify operational Master switch .................................................off Right Wing Flaps .................... security/attach points/linkage Ailerons ................................ movement/security Wingtip/nav lights ............................ undamaged Leading edge condition ................... undamaged Tiedown ................................................. remove Overflow vent ................................ unobstructed Right main gear ........ tire/strut/brakelines/chocks Fuel tank ................................................... sump Fuel quantity................................. check visually Fuel cap ................................ secured/vent clear Nose Engine cowling .................... secure/undamaged Oil level .................................................. 6-8 qts Propeller/spinner .............................undamaged Engine cooling inlets ...................... unobstructed Alternator belt ....................... condition/tightness Air filter inlet................................... unobstructed Nose gear ............. tire inflation/oleo strut/chocks Fuel strainer ..............................................sump Windshield ............................. clean/undamaged Left Wing Fuel tank....................................................sump Fuel quantity ............................................. check Fuel cap ............................... secured/vent clear Left main gear..........tire/strut/brake lines/chocks Tiedown ................................................. remove Overflow vent ................................ unobstructed Pitot/static mast ............................. unobstructed Stall warning switch ....................... moves freely Leading edge condition ....................undamaged Wingtip/nav lights ............................undamaged Ailerons ................................ movement/security Flaps .................... security/attach points/linkage Empennage General surface condition ................undamaged Stabilator ..................movement/security/linkage Rudder (do not move on ground) ........... security Tail tie down .......................................... remove Baggage door ............................... closed/locked Before Startup Passenger briefing ............................... complete Seats/belts/harnesses .............. adjusted/secure Flaps ............................................................. up Flight controls ............................free and correct Fuel selector valve ............................ fullest tank Carburetor heat ............................................. off Avionics switch .............................................. off Engine Start Note: This aircraft does NOT cross feed from both fuel tanks. Fuel tanks must be switched periodically in order to maintain an even fuel load. Brakes .................................................... applied Mixture ........................................................ rich Throttle ........................................... open ¼ inch Master switch ................................................ on Beacon .......................................................... on Electric fuel pump .......................................... on Primer..................................... prime as required Ignition switch ................................ left mag only Prop area........................... clear left/center/right Ignition button ......................... push/hold to start Throttle ............................................... 1000 rpm Oil pressure ..................... normal within 20 secs Ignition switch ............................................. both
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Ammeter ................... ensure alternator charging Mixture .......................... pre-lean for ground ops Avionics ......................................................... on Transponder .................... squawk 1200/standby Electric fuel pump .......................................... off Fuel timer .................................................... start Radios .......... obtain weather and taxi clearance Taxi Brakes ......................................................check IFR taxi check (if needed) Compass............................ swinging freely Turn coordinator ................ opposite of turn Directional gyro ......................... shows turn Attitude indicator .......................... 5mins/5° Ground check/Engine run-up Aircraft ............................. position appropriately Brakes ...................................................... apply Door/window ............................... closed/latched Primer .................................................. in/locked Fuel selector valve ....................... on fullest tank Elevator trim .................................. set to neutral Mixture (lean for density altitude) Mixture ............................................full rich Throttle........................................ 2000 rpm Mixture ... adjust to slightly rich of full power Engine (operational check) Throttle........................................ 2000 rpm Oil pressure/temperature................. normal Alternator ..................................14-15 volts Magnetos ........... 125 rpm drop/run smooth Carburetor heat ...................... check for ice Idle check ............... verify engine operation Throttle ............................................... 1000 rpm Flight instruments ............................ checked/set Radios ................ notify traffic/take-off clearance Before Takeoff Lights ................................................ as needed Transponder .................................................. alt Fuel selector ..................................... fullest tank Electric fuel pump .......................................... on Take-off briefing Engine loss prior to rotation ............. briefed Engine loss after rotation ................. briefed Engine loss above 700’ AGL ........... briefed Runway ............... clear on final/ahead/departure Normal Takeoff Throttle ......................................................... full Rotate .............................................. 65-70 KIAS Initial climb-out ...................................... 75 KIAS Cruise climb .......................................... 87 KIAS Short-field Takeoff Flaps ............................................................ 25° Throttle ......................................................... full Rotate and climb-out (first 100’ agl) ................ 65 Soft-field Takeoff Flaps ............................................................ 25° Throttle ......................................................... full Maintain a slightly nose high attitude until the aircraft leaves the runway Climb-out (above 100’ agl and clear of all obstacles) Flaps .................................. retract incrementally Engine gauges ......................................... check Airspeed ............................................... 87 KIAS Cruise Throttle ............................................... 2500 rpm Mixture .......................... re-lean every 3000’ msl Heading indicator/compass............... crosscheck Landing/Taxi lights......................................... off Electric boost pump ........... off above 1000’ AGL Switching fuel tanks Aircraft ..................................... straight and level Electric boost pump ....................................... on Fuel selector switch ........................ to other tank Fuel pressure/flow ............ stable for 30 seconds Electric boost pump ....................................... off Descent/Landing Seatbelts and harnesses ......................... secure Electric boost pump ....................................... on Fuel selector ..................................... fullest tank Throttle ........................................app. 1500 rpm Mixture ................................... enrich as needed Flaps ................................................. as desired Airspeed .............................. 75-80 KIAS on final Carburetor heat ................................. as needed After Landing Runway ........................................... clear/exited Flaps ............................................................. up Lights (except beacon) ...................... as needed Fuel pump ..................................................... off Elevator trim ........................................... neutral Carburetor heat ................................. as needed Radios ........................... obtain clearance to taxi Shutdown Lights (except beacon) .................................. off Avionics switch .............................................. off Mixture .................................................. full lean Ignition switch ................................................ off Master switch ................................................ off Hobbs & tach time ................................... record Trash & personal items ....... removed from plane Aircraft ...................tied down/in hangar/chocked Leading edges/surfaces..................... wipe down Dispatch status ...................... filled out/complete WARNING: The information required to be in any checklist varies between individual aircraft. The information in this checklist constitutes only partial information and is not to be used as a substitute for the information contained in the approved pilot’s operating handbook. Use of this checklist indicates that the user assumes all risk of use and consents to bear all liability associated with the use of this product. AV-30C Set altimeter Button 2............... press until ‘1:3’ page is visible Knob ..................... press once to select altimeter .................. rotate knob to change altimeter ......................... press again to save setting Set heading Button 2............... press until ‘1:3’ page is visible Knob ..................... press twice to select heading ................... rotate knob to change heading ......................... press again to save setting Set transponder code/mode Button 2.................press until ‘AI’ page is visible Knob ........................... press to enter ‘edit’ mode .....................rotate to select/modify digit(s) Button 2........ press to set xpdr mode (if needed) Button 1.......................... press to save changes Button 1 Knob Button 2 WARNING This device was configured upon installation. Entering the setup menu is forbidden. Do NOT attempt to change the fields or reconfigure the device. Page